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FR2974150B1 - Inverseur de poussee pour turboreacteur d'aeronef - Google Patents

Inverseur de poussee pour turboreacteur d'aeronef

Info

Publication number
FR2974150B1
FR2974150B1 FR1101160A FR1101160A FR2974150B1 FR 2974150 B1 FR2974150 B1 FR 2974150B1 FR 1101160 A FR1101160 A FR 1101160A FR 1101160 A FR1101160 A FR 1101160A FR 2974150 B1 FR2974150 B1 FR 2974150B1
Authority
FR
France
Prior art keywords
actuator
cowl
vanes
deflecting
slideways
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1101160A
Other languages
English (en)
Other versions
FR2974150A1 (fr
Inventor
Nicolas Dezeustre
Olivier Kerbler
Herve Hurlin
Casellas Pierre Moradell
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Nacelles SAS
Original Assignee
Aircelle SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR1101160A priority Critical patent/FR2974150B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to CA2831187A priority patent/CA2831187A1/fr
Priority to CN201280018364.1A priority patent/CN103492696A/zh
Priority to EP12721330.4A priority patent/EP2697497B1/fr
Priority to RU2013150007/06A priority patent/RU2013150007A/ru
Priority to BR112013024873A priority patent/BR112013024873A2/pt
Priority to PCT/FR2012/050796 priority patent/WO2012140368A1/fr
Publication of FR2974150A1 publication Critical patent/FR2974150A1/fr
Application granted granted Critical
Publication of FR2974150B1 publication Critical patent/FR2974150B1/fr
Priority to US14/048,206 priority patent/US9458793B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
    • F02K1/625—Reversing jet main flow by blocking the rearward discharge by means of flaps the aft end of the engine cowling being movable to uncover openings for the reversed flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/34—Arrangement of components translated
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Transmission Devices (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Wind Motors (AREA)
  • Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
FR1101160A 2011-04-14 2011-04-14 Inverseur de poussee pour turboreacteur d'aeronef Active FR2974150B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1101160A FR2974150B1 (fr) 2011-04-14 2011-04-14 Inverseur de poussee pour turboreacteur d'aeronef
CN201280018364.1A CN103492696A (zh) 2011-04-14 2012-04-12 用于航空器喷气发动机的推力反向器
EP12721330.4A EP2697497B1 (fr) 2011-04-14 2012-04-12 Inverseur de poussée pour turboréacteur d'aéronef
RU2013150007/06A RU2013150007A (ru) 2011-04-14 2012-04-12 Реверсор тяги для реактивного двигателя летательного аппарата
CA2831187A CA2831187A1 (fr) 2011-04-14 2012-04-12 Inverseur de poussee pour turboreacteur d'aeronef
BR112013024873A BR112013024873A2 (pt) 2011-04-14 2012-04-12 conjunto compreendendo um pylon de suspensão e um reversor de empuxo compreendendo pás
PCT/FR2012/050796 WO2012140368A1 (fr) 2011-04-14 2012-04-12 Inverseur de poussée pour turboréacteur d'aéronef
US14/048,206 US9458793B2 (en) 2011-04-14 2013-10-08 Thrust reverser for an aircraft jet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1101160A FR2974150B1 (fr) 2011-04-14 2011-04-14 Inverseur de poussee pour turboreacteur d'aeronef

Publications (2)

Publication Number Publication Date
FR2974150A1 FR2974150A1 (fr) 2012-10-19
FR2974150B1 true FR2974150B1 (fr) 2013-04-12

Family

ID=46085658

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1101160A Active FR2974150B1 (fr) 2011-04-14 2011-04-14 Inverseur de poussee pour turboreacteur d'aeronef

Country Status (8)

Country Link
US (1) US9458793B2 (fr)
EP (1) EP2697497B1 (fr)
CN (1) CN103492696A (fr)
BR (1) BR112013024873A2 (fr)
CA (1) CA2831187A1 (fr)
FR (1) FR2974150B1 (fr)
RU (1) RU2013150007A (fr)
WO (1) WO2012140368A1 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2999240B1 (fr) * 2012-12-11 2015-01-02 Aircelle Sa Systeme de synchronisation pour dispositif d'inversion de poussee
FR2999155B1 (fr) * 2012-12-12 2014-11-21 Aircelle Sa Ensemble propulsif pour aeronef
CN103112595B (zh) * 2013-02-06 2016-01-27 中国商用飞机有限责任公司 推进系统一体化的吊挂结构
WO2015069350A2 (fr) * 2013-08-28 2015-05-14 United Technologies Corporation Ensemble porte coulissante à inverseur de poussée
FR3020344B1 (fr) * 2014-04-24 2016-05-13 Airbus Operations Sas Assemblage pour un aeronef comportant un panneau d'acces mobile
US9410501B2 (en) * 2014-04-25 2016-08-09 Rohr, Inc. Translating sleeve actuation system and apparatus
FR3028295B1 (fr) * 2014-11-06 2020-01-17 Safran Electronics & Defense Systeme d'actionnement d'une structure mobile d'un inverseur de poussee d'un aeronef, inverseur de poussee et reacteur comprenant un tel systeme.
FR3031726B1 (fr) * 2015-01-21 2017-02-24 Aircelle Sa Systeme pour la pose et la depose d’un ensemble propulsif sur un mat d’un aeronef
US10267262B2 (en) * 2016-05-06 2019-04-23 Mra Systems, Llc Thrust reverser assembly
FR3067406B1 (fr) * 2017-06-13 2019-07-12 Airbus Operations Systeme d'inverseur de poussee presentant des perturbations aerodynamiques limitees
CN109026436A (zh) * 2018-08-22 2018-12-18 中国商用飞机有限责任公司 反推作动装置及涡轮喷气发动机短舱
FR3100577B1 (fr) * 2019-09-05 2021-12-03 Safran Nacelles Inverseur de poussée comprenant un unique vérin de commande de capot mobile
FR3100578B1 (fr) 2019-09-05 2021-09-24 Safran Nacelles Inverseur de poussée muni d’une cinématique à câble pour volets écopants
FR3100576B1 (fr) * 2019-09-05 2021-09-17 Safran Nacelles Inverseur de poussée comprenant des verrous primaires décalés par rapport à un plan de symétrie du capot mobile
IT202000013846A1 (it) * 2020-06-10 2021-12-10 Leonardo Spa Inversore di spinta per sistema propulsivo turboventola di aeromobile, e relativi sistema propulsivo turboventola e metodo di inversione di spinta
CN114684384B (zh) * 2020-12-25 2023-11-17 中国科学院沈阳自动化研究所 一种飞机发动机的安装装置及安装方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3503211A (en) * 1968-04-10 1970-03-31 Rohr Corp Thrust reverser
US3500644A (en) * 1968-04-10 1970-03-17 Rohr Corp Thrust reverser
GB1418905A (en) * 1972-05-09 1975-12-24 Rolls Royce Gas turbine engines
US4998409A (en) * 1989-09-25 1991-03-12 Rohr Industries, Inc. Thrust reverser torque ring
FR2669679B1 (fr) * 1990-11-28 1994-04-29 Sud Ouest Conception Aeronauti Tuyere d'ejection de gaz pour moteur a reaction et moteur a reaction equipe d'une telle tuyere, en particulier moteur du type a flux separes.
US6340135B1 (en) * 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine
FR2821892B1 (fr) * 2001-03-08 2003-06-13 Hispano Suiza Sa Systeme d'actionnement du capotage mobile d'un inverseur de poussee dans un turboreacteur
US6584763B2 (en) * 2001-08-01 2003-07-01 Rohr, Inc. Lock for the translating sleeve of a turbofan engine thrust reverser
US7484356B1 (en) * 2005-07-26 2009-02-03 Aeronautical Concepts Of Exhaust, Llc Cascade reverser without blocker doors
FR2916426B1 (fr) 2007-05-22 2010-04-02 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur.
FR2921976B1 (fr) * 2007-10-08 2009-12-04 Aircelle Sa Actionneur pour structure mobile de nacelle d'aeronef, et nacelle comprenant au moins un tel actionneur
FR2932226B1 (fr) * 2008-06-06 2013-08-23 Aircelle Sa Procede de synchronisation des actionneurs d'un capot mobile d'inverseur de poussee
FR2966882B1 (fr) * 2010-11-03 2017-10-27 Aircelle Sa Inverseur de poussee pour turboreacteur d'aeronef a nombre d'actionneurs reduit

Also Published As

Publication number Publication date
CN103492696A (zh) 2014-01-01
RU2013150007A (ru) 2015-05-20
WO2012140368A1 (fr) 2012-10-18
US9458793B2 (en) 2016-10-04
FR2974150A1 (fr) 2012-10-19
EP2697497A1 (fr) 2014-02-19
EP2697497B1 (fr) 2019-08-07
US20140061332A1 (en) 2014-03-06
BR112013024873A2 (pt) 2016-12-20
CA2831187A1 (fr) 2012-10-18

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